MakeItFrom.com
Menu (ESC)

ASTM A182 Grade F92 vs. 6013 Aluminum

ASTM A182 grade F92 belongs to the iron alloys classification, while 6013 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is ASTM A182 grade F92 and the bottom bar is 6013 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 22
3.4 to 22
Fatigue Strength, MPa 360
98 to 140
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 440
190 to 240
Tensile Strength: Ultimate (UTS), MPa 690
310 to 410
Tensile Strength: Yield (Proof), MPa 500
170 to 350

Thermal Properties

Latent Heat of Fusion, J/g 260
410
Maximum Temperature: Mechanical, °C 590
160
Melting Completion (Liquidus), °C 1490
650
Melting Onset (Solidus), °C 1450
580
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 26
150
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.3
38
Electrical Conductivity: Equal Weight (Specific), % IACS 10
120

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.9
2.8
Embodied Carbon, kg CO2/kg material 2.8
8.3
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 89
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
13 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 650
200 to 900
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
49
Strength to Weight: Axial, points 24
31 to 41
Strength to Weight: Bending, points 22
37 to 44
Thermal Diffusivity, mm2/s 6.9
60
Thermal Shock Resistance, points 19
14 to 18

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0 to 0.020
94.8 to 97.8
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.070 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0 to 0.1
Copper (Cu), % 0
0.6 to 1.1
Iron (Fe), % 85.8 to 89.1
0 to 0.5
Magnesium (Mg), % 0
0.8 to 1.2
Manganese (Mn), % 0.3 to 0.6
0.2 to 0.8
Molybdenum (Mo), % 0.3 to 0.6
0
Nickel (Ni), % 0 to 0.4
0
Niobium (Nb), % 0.040 to 0.090
0
Nitrogen (N), % 0.030 to 0.070
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0.6 to 1.0
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.1
Tungsten (W), % 1.5 to 2.0
0
Vanadium (V), % 0.15 to 0.25
0
Zinc (Zn), % 0
0 to 0.25
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.15